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  • MIL-D-8684 Revision B:1959

    Withdrawn A Withdrawn Standard is one, which is removed from sale, and its unique number can no longer be used. The Standard can be withdrawn and not replaced, or it can be withdrawn and replaced by a Standard with a different number.

    DATA AND TESTS, ENGINEERING, CONTACT REQUIREMENTS FOR AIR LAUNCHED GUIDED MISSILE SYSTEMS

    Available format(s):  PDF

    Withdrawn date:  28-08-1996

    Language(s):  English

    Published date: 

    Publisher:  US Military Specs/Standards/Handbooks

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    Abstract - (Show below) - (Hide below)

    Covers requirements for engineering data and tests to be furnished under contracts for air launched guided missile systems.

    General Product Information - (Show below) - (Hide below)

    Committee FSC 14GP
    Document Type Standard
    Publisher US Military Specs/Standards/Handbooks
    Status Withdrawn

    Standards Referenced By This Book - (Show below) - (Hide below)

    MIL-STD-1606 Revision A:1983 TECHNICAL INFORMATION REQUIREMENTS FOR AIR LAUNCHED GUIDED MISSILE PROPOSALS

    Standards Referencing This Book - (Show below) - (Hide below)

    MIL STD 1304 : A RELIABILITY AND MAINTAINABILITY ENGINEERING DATA
    MIL-I-8500 Revision D:1980 INTERCHANGEABILITY AND REPLACEABILITY OF COMPONENT PARTS FOR AEROSPACE VEHICLES
    MIL D 5480 : F DATA, ENGINEERING AND TECHNICAL REPRODUCTION REQUIREMENTS FOR
    MIL M 8910 : NOTICE 1 MANUALS, TECHNICAL, ILLUSTRATED PARTS BREAKDOWN
    MIL-STD-704 Revision F:2004 AIRCRAFT ELECTRIC POWER CHARACTERISTICS
    MIL-H-25475 Revision B:1971 HYDRAULIC SYSTEM, MISSILE, DESIGN, INSTALLATION TESTS AND DATE REQUIREMENTS, GENERAL REQUIREMENTS FOR
    MIL-A-8870 Revision C:1993 AIRPLANE STRENGTH AND RIGIDITY VIBRATION, FLUTTER, AND DIVERGENCE
    MIL-E-7016 Revision F:1976 ELECTRIC LOAD AND POWER SOURCE CAPACITY, AIRCRAFT ANALYSIS OF
    MIL STD 15 : (2) ELECTRICAL WIRING EQUIPMENT SYMBOLS FOR SHIPS PLANS PART 2
    MIL E 5400 : T ELECTRONIC EQUIPMENT, AEROSPACE, GENERAL SPECIFICATION FOR
    MIL-W-3947 Revision B:1969 WEIGHT AND BALANCE CONTROL SYSTEM FOR GUIDED MISSILES AND SPACE LAUNCH VEHICLES
    MIL-STD-838 Revision C:1983 LUBRICATION OF MILITARY EQUIPMENT
    MIL-STD-176 Revision A:1963 GUIDED MISSILES AND SPACE LAUNCH VEHICLES, WEIGHT AND BALANCE DATA REPORTING FORMS FOR
    MIL-A-8868 Revision B:1987 AIRPLANE STRENGTH AND RIGIDITY DATA AND REPORTS
    MIL-T-5422 Revision F:1971 TESTING, ENVIRONMENTAL, AIRCRAFT ELECTRONIC EQUIPMENT
    MIL S 901 : D SHOCK TESTS, HI [HIGH IMPACT] SHIPBOARD MACHINERY, EQUIPMENT AND SYSTEMS, REQUIREMENTS FOR
    MIL-P-25062 Revision B:1964 PARACHUTE RECOVERY SYSTEM, MISSILE AND DRONE, GENERAL REQUIREMENT FOR DEVELOPMENT OF
    MIL-STD-100 Revision G:1997 ENGINEERING DRAWINGS
    MIL-D-18300 Revision H:1993 DESIGN EXAMINATIONS, ENGINEERING AVIONIC SYSTEMS/EQUIPMENT GENERAL REQUIREMENTS FOR
    MIL-STD-167 Base Document:1993 MECHANICAL VIBRATIONS OF SHIPBOARD EQUIPMENT
    MIL-E-8189 Revision H:1975 ELECTRONIC EQUIPMENT, MISSILES, BOOSTERS AND ALLIED VEHICLES, GENERAL SPECIFICATION FOR
    MIL-D-23660 Revision A:1965 DATA, TECHNICAL FOR ROCKET MOTORS
    MIL D 1000/1 : LATEST DRAWING, ENGINEERING & ASSOCIATED DATA
    MIL-D-18243 Revision B:1977 DEMONSTRATION OF AIRBORNE TARGET AND MISSILE SYSTEMS GENERAL SPECIFICATION FOR
    MIL-F-7179 Revision G:1993 FINISHES, COATINGS, AND SEALANTS FOR THE PROTECTION OF AEROSPACE WEAPONS SYSTEM
    MIL-S-23069 Revision A:1983 SAFETY REQUIREMENTS, MINIMUM, FOR AIR LAUNCHED GUIDED MISSILES
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